Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:application |
Conventional runway takeoff and landing
|
| gptkbp:capacity |
350 kg (Rustom-2)
|
| gptkbp:countryOfOrigin |
gptkb:India
|
| gptkbp:developedBy |
gptkb:Defence_Research_and_Development_Organisation
|
| gptkbp:endurance |
12-24 hours
|
| gptkbp:engineType |
Piston engine
|
| gptkbp:firstFlight |
2010
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rustom UAV
|
| gptkbp:namedAfter |
gptkb:Rustom_Damania
|
| gptkbp:role |
Surveillance
Reconnaissance Intelligence gathering |
| gptkbp:status |
Under development
|
| gptkbp:type |
Medium-altitude long-endurance UAV
|
| gptkbp:usedBy |
gptkb:Indian_Armed_Forces
|
| gptkbp:variant |
gptkb:Rustom-1
gptkb:Rustom-2 gptkb:Rustom-H |
| gptkbp:wingspan |
20.6 m (Rustom-2)
7.9 m (Rustom-1) |
| gptkbp:bfsParent |
gptkb:Defence_Research_and_Development_Organisation
|
| gptkbp:bfsLayer |
5
|